Platform Balance

ABSTRACT

In one aspect, a platform balance includes a frame support, and at least three spaced-apart transducer bodies coupled to the frame support. Each transducer body includes a support having clevis halves. The sensor body includes a generally rigid peripheral member disposed about a spaced-apart central hub joined to each of the clevis halves. At least three flexure components couple the peripheral member to the hub. The flexure components are spaced-apart from each other at generally equal angle intervals about the hub; the sensor body further including a flexure assembly for some flexure components joining the flexure component to at least one of the hub and the peripheral member, the flexure assembly being compliant for forces in a radial direction from the hub to the peripheral member. Each flexure assembly is configured such that forces transferred concentrate strain at a midpoint along the length of each corresponding flexure component.

CROSS-REFERENCE TO RELATED APPLICATION

This application claims the benefit of U.S. Provisional patentapplication Ser. No. 61/861,221, entitled “TWO-AXIS SENSOR BODY FOR ALOAD TRANSDUCER” filed Aug. 1, 2013, and U.S. Provisional patentapplication Ser. No. 62/031,642, entitled “TWO-AXIS SENSOR BODY FOR ALOAD TRANSDUCER” filed Jul. 31, 2014, the contents of each of which areincorporated herein by reference in their entireties.

BACKGROUND OF THE INVENTION

The discussion below is merely provided for general backgroundinformation and is not intended to be used as an aid in determining thescope of the claimed subject matter.

The present disclosure relates to devices that transmit and measurelinear forces along and moments about three orthogonal axes. Moreparticularly, the present disclosure relates to devices that areparticularly well suited to measure forces and moments upon a testspecimen in a test environment, such as but not limited to in a windtunnel.

The measurement of loads, both forces and moments, with accuracy andprecision is important to many applications. A common use, where severalmoments and forces need to be measured, is in the testing of specimensin a wind tunnel. Test specimens can be placed on a platform balancelocated in a pit of the wind tunnel. The platform balance can bearranged to receive a model of a vehicle, a vehicle, or other actual ormodeled test specimen.

If the test specimen is a vehicle with wheels, the platform balance canbe equipped with a rolling belt to rotate the wheels, which can make asignificant improvement in measurement accuracy.

Six components of force and moment act on a test specimen on theplatform balance in the wind tunnel. These six components are known aslift force, drag force, side force, pitching moment, yawing moment, androlling moment. The moments and forces that act on the test specimen areusually resolved into three components of force and three components ofmoment with transducers that are sensitive to the components. Each ofthe transducers carries sensors, such as strain gauges, that areconnected in combinations that form Wheatstone bridge circuits. Byappropriately connecting the sensors, resulting Wheatstone bridgecircuit unbalances can be resolved into readings of the three componentsof force and three components of moment.

Platform balances have a tendency to be susceptible to various physicalproperties of the test environment that can lead to inaccuratemeasurements without additional compensation. For example, temperaturetransients in the wind tunnel can result in thermal expansion of theplatform balance that can adversely affect the transducers. In addition,large test specimens are prone to create large thrust loads on thetransducers that can cause inaccurate measurements.

SUMMARY

This Summary and the Abstract herein are provided to introduce aselection of concepts in a simplified form that are further describedbelow in the Detailed Description. This Summary and the Abstract are notintended to identify key features or essential features of the claimedsubject matter, nor are they intended to be used as an aid indetermining the scope of the claimed subject matter. The claimed subjectmatter is not limited to implementations that solve any or alldisadvantages noted in the Background.

An aspect of the invention provides a platform balance suitable fortransmitting forces and moments in a plurality of directions, theplatform balance including a frame support, and at least threespaced-apart transducer bodies coupled to the frame support. Eachtransducer body includes a support comprising a pair of clevis halves;and a sensor body coupled to each of the clevis halves, wherein thesensor body is disposed between the clevis halves and configured todeflect with forces along two orthogonal axes, wherein the sensor bodyincludes a generally rigid peripheral member disposed about aspaced-apart central hub, the central hub being joined to each of theclevis halves with the peripheral member spaced apart from each clevishalf, wherein at least three flexure components couple the peripheralmember to the central hub, and wherein the flexure components arespaced-apart from each other at generally equal angle intervals aboutthe central hub; the sensor body further including a flexure assemblyfor each of said at least some flexure components joining the flexurecomponent to at least one of the central hub and the peripheral member,the flexure assembly being compliant for forces in a radial directionfrom the central hub through the flexure component and to the peripheralmember, wherein each flexure assembly is configured such that forcestransferred between central hub and the peripheral member concentratestrain at a midpoint along the length of each corresponding flexurecomponent.

An aspect of the invention provides a platform balance suitable fortransmitting forces and moments in a plurality of directions, theplatform balance including a frame support, and at least threespaced-apart transducer bodies coupled to the frame support. Eachtransducer body includes a support comprising a pair of clevis halves; asensor body coupled to each of the clevis halves, wherein the sensorbody is disposed between the clevis halves and includes a generallyrigid peripheral member disposed about a spaced-apart central hub, thecentral hub being joined to each of the clevis halves with theperipheral member spaced apart from each clevis halve, wherein at leastthree flexure components couple the peripheral member to the centralhub, and wherein the flexure components are spaced-apart from each otherat generally equal angle intervals about the central hub; and a biasingassembly connected between the support and the sensor body andconfigured to provide a bias force between the sensor body and thesupport.

Another aspect of the invention provides An aspect of the inventionprovides a platform balance suitable for transmitting forces and momentsin a plurality of directions, the platform balance including a framesupport, and at least three spaced-apart transducer bodies coupled tothe frame support. Each transducer body includes a support comprising apair of clevis halves; a sensor body coupled to each of the clevishalves, wherein the sensor body is disposed between the clevis halvesand includes a generally rigid peripheral member disposed about aspaced-apart central hub, the central hub being joined to each of theclevis halves with the peripheral member spaced apart from each clevishalve, wherein at least three flexure components couple the peripheralmember to the central hub, and wherein the flexure components arespaced-apart from each other at generally equal angle intervals aboutthe central hub; and a lockup assembly configured to selectively inhibitmovement of the sensor body relative to the clevis halves.

Additional aspects of the invention may be combined with any of theabove aspects and with each other. Such additional aspects include thefollowing:

An aspect wherein each flexure assembly is configured such that forcestransferred between central hub and the peripheral member cause a firstforce at the connection of the flexure component to the central hub tobe equal and opposite to a second force at the connection of the flexurecomponent to the peripheral member, wherein the first and second forceare tangential to the radial direction of each corresponding flexurecomponent.

An aspect wherein said at least some of the flexure components areconfigured to concentrate strain in shear.

An aspect wherein said at least some of the flexure components areconfigured to concentrate strain in bending.

An aspect wherein said at least some of the flexure components areconfigured with a pair of beams.

An aspect wherein the pair of beams of each flexure component of atleast some of the flexure components is formed by an aperture.

An aspect wherein the biasing assembly comprises a bias connectorconfigured to operate in tension to provide the bias force.

An aspect wherein the bias connecter comprises an elongated strap havinga width of the strap greater than a thickness of the strap.

An aspect wherein the biasing assembly comprises a pair of strapsprovided on opposite portions of the transducer body that aresymmetrical.

An aspect wherein the bias connector comprises a flexible member fixedlyconnected to one of the sensor body or the support.

An aspect wherein the flexible member is integrally formed from a singleunitary body of one of the sensor body or the support.

An aspect wherein the biasing assembly comprises a pair of biasingconnectors wherein a biasing connector is provided each of oppositeportions of the transducer body that are symmetrical.

An aspect wherein the biasing assembly comprises flexible members, aflexible member being fixedly connected to one of the sensor body or thesupport.

An aspect wherein the flexible members are integrally formed from asingle unitary body of one of the sensor body or the support.

An aspect wherein each flexible member comprises a cantilevered beamwith one of the biasing connectors connected to one of the flexiblemembers.

An aspect wherein the flexible member is provided on the support.

An aspect wherein a flexible member is provided on each clevis half anda bridging block connects the flexible members together, the bridgingblock being spaced apart from the sensor body.

An aspect wherein the flexible member is provided on the sensor body.

An aspect wherein the biasing assembly comprises a removable biasingactuator configured to be connected between the sensor body and thesupport.

An aspect wherein the lockup assembly is configured to inhibit movementof the peripheral member relative to the clevis halves.

An aspect wherein the lockup assembly inhibits movement of theperipheral member by frictional contact.

An aspect wherein the lockup assembly is configured to selectively moveportions having engaging surfaces for frictional contact to contactopposed surfaces of the peripheral member, the engaging surfaces and theopposed surfaces being spaced apart from each other to allow forces tobe transferred by the flexure components when the lockup assembly is notengaged.

An aspect wherein the lockup assembly comprises a first plate memberjointed to a first clevis half and a second plate member joined to thesecond clevis halve, wherein the engaging surfaces are disposed on theplate members.

An aspect wherein a portion of each plate member is space apart from theassociated clevis half.

An aspect wherein when the engaging surface engage the opposed surfaces,the portion of each plate member frictionally engages the associatedclevis half.

An aspect and further comprising an actuator configured to selectivelybring the engaging surfaces in contact with the opposed surfaces andalso bring the portions of each plate member into contact with eachassociated clevis half.

An aspect wherein major surfaces of the portions of the plate membersengage major surfaces of the associated clevis halves.

An aspect wherein the engaging surfaces are on the plate members, andwherein each plate member comprises a hinges and a link portion betweenthe hinges, the link portion connecting portions of the plate membershaving the engaging surfaces with portions of the plate members havingthe major surfaces.

An aspect wherein the actuator is operably mounted to the portions ofthe plate members having the engaging surfaces, and wherein the actuatorincludes a pull rod to selectively pull the pull rod so as to bring theengaging surfaces in contact with the opposed surfaces.

An aspect wherein the pull rod extends through a bore opening to one ofthe opposed surfaces, the pull rod being spaced apart from innersurfaces of the bore at least when the actuator is not pulling on thepull rod to bring the engaging surfaces in contact with the opposedsurfaces.

A platform balance may be provided in another aspect with transducerbodies and aspects as shown and described.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a side elevation view of a transducer body according to anembodiment of the present disclosure;

FIG. 2 is a perspective view of a sensor body according to an embodimentof the present disclosure;

FIG. 3 is a front elevation view of the sensor body of FIG. 2;

FIG. 4 is a view of the sensor body taken along lines 4-4 of FIG. 3;

FIG. 5 is a close-up view of a portion of the sensor body of FIG. 3;

FIG. 6 is a close-up view of a portion of the cut away view of FIG. 4;

FIG. 7 is a circuit diagram of a Wheatstone bridge for the sensorelements of FIG. 2;

FIG. 8 is a close up view of a portion of the sensor body of FIG. 2;

FIG. 9 is a front elevation view of a sensor body according to anotherembodiment of the present disclosure;

FIG. 10 is a perspective view of the sensor body of FIG. 9;

FIG. 11 is a close up view of a portion of the sensor body of FIG. 10;

FIG. 12 is a front elevation view showing locations of sensor elementson the sensor body of FIG. 9;

FIG. 13 is a circuit diagram of a Wheatstone bridge for the sensorelements of FIG. 9;

FIG. 14 is a front elevation view of a sensor body according to anotherembodiment of the present disclosure;

FIG. 15 is a close up view of a flexure element of the sensor body ofthe FIG. 14;

FIG. 16 is a front elevation view of yet another sensor body accordingto another embodiment of the present disclosure;

FIG. 17 is a bottom view of the sensor body of FIG. 16;

FIG. 18 is a perspective view of the sensor body of FIG. 16;

FIG. 19 is a cut away view along lines 19-19 of FIG. 16;

FIG. 20 is a close up view of a flexure element of FIG. 16;

FIG. 21 is a close up view of an alternate flexure element according toanother embodiment of the present disclosure;

FIG. 22 is a top view of a platform balance according to an embodimentof the present disclosure;

FIG. 23 is a side elevation view of the platform balance of FIG. 22;

FIG. 24 is a perspective view of a transducer body according to anotherembodiment of the present disclosure;

FIG. 25 is a front elevation view of the transducer body of FIG. 24;

FIG. 26 is a perspective view of a transducer body according to anotherembodiment of the present disclosure;

FIG. 27 is a front elevation view of the assembly of FIG. 26;

FIG. 28 is a right side elevation of the assembly of FIG. 26;

FIG. 29 is a cut away view showing a front elevation of a sensor body inplace on the assembly of FIG. 26;

FIG. 30 is a close up view of a portion of FIG. 29;

FIG. 31 is a perspective view of a clamp assembly in place on atransducer body according to another embodiment of the presentdisclosure;

FIG. 32 is a close up and partial cut away view of a portion of theassembly of FIG. 31;

FIG. 33 is a perspective view of a transducer body in a fluidrecirculating bath assembly according to another embodiment of thepresent disclosure; and

FIG. 34 is a front elevation view of the assembly of FIG. 33.

DETAILED DESCRIPTION OF THE ILLUSTRATIVE EMBODIMENTS

Referring to FIG. 1, a transducer assembly is illustrated at 10. Thetransducer assembly 10 includes a sensor body 12 and a clevis assembly14. The clevis assembly 14 includes a first clevis half 16 and a secondclevis half 18. The clevis halves 16 and 18 are joined together at oneend with a connecting member 17. The sensor body 12 is disposed betweenthe clevis halves 16 and 18, where the sensor body 12 and clevis halves16 and 18 are joined together with a suitable fastener assembly. In theembodiment illustrated, the sensor body 12 includes a plurality ofapertures 15 (FIG. 2) through which bolts or threaded rods can extendtherethrough so as to secure each of the clevis halves 16 and 18 (havingsimilar aligned apertures) to opposite sides of the sensor body 12. Inanother embodiment, a bolt or threaded rod can extend through alignedbores 19, 21, and 23 (FIG. 1) in each of the clevis halves 16 and 18 andsensor body 12. A nut (not shown) can be provided on one end of the rodand a super nut can be threaded upon an opposite end. A plurality of setscrews extends though apertures in the super nut to engage in end of oneof the clevis halves 16 or 18. This fastening technique is described inU.S. Pat. No. 7,788,984, which is incorporated herein by reference inits entirety.

It should be noted that although portions of the clevis 16 and 18 willengage or contact a center portion of the sensor body 12, gaps areprovided between each of the clevis halves 16 and 18 and the sensor body12 so as to allow portions of the sensor body 12 to move relative to theclevis halves 16 and 18. In the embodiment illustrated, projectingcenter portions 15A and 15B provided on each side of the sensor body 12ensure contact of the clevis halves 16, 18 only with the center portions15A and 15B (FIGS. 3 and 4), thereby maintaining the gaps as describedabove.

Referring to FIGS. 2-6, the sensor body 12 is preferably integral, beingformed of a signal unitary block of material. The sensor body 12includes a rigid central hub 20 upon which the surfaces 15A and 15Breside, and a rigid perimeter body 22 that is concentric with ordisposed about central hub 20. A plurality of flexure structures 24 jointhe central hub 20 to the perimeter body 22. In the embodimentillustrated, the plurality of flexure structures 24 comprise fourcomponents 31, 32, 33 and 34. Each of the components 31-34 extendradially from the central hub 20 along corresponding longitudinal axis31A, 32A, 33A and 34A. Preferably, axis 31A is aligned with axis 33A,while axis 32A is aligned with axis 34A. In addition, axes 31A and 33Aare perpendicular to axes 32A and 34A. Although illustrated wherein theplurality of flexure components equals four, it should be understoodthat any number of components three or more can be used to join thecentral hub 20 to perimeter body 22. Preferably, the flexure components31-34 are spaced at equal angular intervals about a central axisindicated at 35.

Referring to flexure component 31 by way of example, an intermediatemember 41 is integral with, being formed from the unitary block ofmaterial, or otherwise connected to flexure component 31 at an endopposite central hub 20. Intermediate member 41 is preferably symmetricwith respect to flexure component 31 or longitudinal axis 31A havingside portions 41A and 41B on opposite sides of flexure component 31 orlongitudinal axis 31A. Each side portion 41A, 41B is connected toperimeter body 22 through a flexure assembly 51A, 51B, respectively.Referring to flexure assembly 51A by way of example, each of the flexureassemblies 51A and 51B, in the embodiment illustrated, include a rigidconnecting member 55. The connecting member 53 is connected or joined toone of the side portions 41A, 41B through a thin flexible web 55. At anend opposite the intermediate member 41, the connecting member 55 isconnected to perimeter body 22 through a thin web 57. It should be notedthat the webs 55 and 57 are relatively wide being, for example, similarto the width or thickness of the perimeter body 22; however, each of thewebs 55 and 57 are thin in a direction normal to the width of theperimeter body 22. The orientation of each of the webs 55 and 57connecting the intermediate member 41 to the perimeter body 22 areoriented perpendicular to the flexure component associated with eachintermediate number 41. In other words, each of the connecting webs 55and 57 are relatively wide in a direction parallel to the central axis35, but thin in a cross-section perpendicular to axis 35. In contrast,each of the flexure components 31-34 are thin in a direction parallel tothe central axis 35 and relatively wide in a cross-section perpendicularto the axis 35. Given this construction, the connecting webs 55 and 57are compliant for forces along the longitudinal axis of the flexurecomponent to which it is connected, but stiff for an axis orthogonal tothe axis of the flexure component to which it is associated with, andthe axis orthogonal to the foregoing axes (or the axis parallel to thecentral axis 35).

In the exemplary embodiment comprising four orthogonal flexurecomponents 31-34, the flexure components 31-34 operate in pairs forforces along an axis that is orthogonal to the longitudinal axes of eachpair of flexure components (31,33 and 32,34) and orthogonal to thecentral axis 35. In particular, flexure components 31 and 33 transferforces between the central body 20 and the perimeter body 22 for forcesalong an axis 61 (wherein connecting webs 55 and 57 associated flexurecomponents 32 and 34 are compliant in this direction), while flexurecomponents 32 and 34 transfer forces between the central body 20 and theperimeter body 22 for forces along an axis 63 (wherein connecting webs55 and 57 associated flexure components 31 and 33 are compliant in thisdirection).

It should be noted that the flexure assemblies 51A and 51B (herein byexample connecting member 53 and connecting webs 55, 57) associated witheach flexure component 31-34 (on opposite sides of the flexurecomponent) are disposed so as to coincide at least approximately with amidpoint along the length of the corresponding flexure component.Referring to the enlarged view of FIG. 5 a midpoint of the longitudinallength of the flexure component 31 is indicated at 66. The flexureassemblies 51A, 51B on opposite sides of the flexure component 31(herein comprising connecting webs 55 and 57), are orthogonal to theassociated flexure component in a planar sense, but are configured ordisposed so as to be approximately inline with the midpoint 66 asrepresented by dashed line 68, or substantially proximate to themidpoint 66. In other words the web(s) of the flexure assemblies 51A,51B on each side of the flexure component they are associated with canbe defined by corresponding planes, the planes of which are orthogonalto a plane representing the flexure component. Orientation of theconnecting web(s) of the flexure assemblies 51A, 51B relative to theassociated flexure component at the midpoint 66 causes forces to betransferred through the center of the length of the flexure componentwhich allows the component to be very stiff with most deflection due tostrain deflection and not bending. Since the flexure component is verystiff it has a good frequency response with excellent resolution. Sinceeach of the flexure components 31-34 and associated flexure assemblies51A, 51B are connected in the manner described above about center axis35, the sensor body 12 includes flexure elements (flexure components31-34) that can be used to sense forces with respect to two orthogonalaxes 61, 63 that can carry high loads with high resolution.

In one embodiment, each flexure assembly is configured such that forcestransferred between central hub 20 and the peripheral member 22 cause afirst force at the connection of the flexure component to the centralhub 20 to be equal and opposite to a second force at the connection ofthe flexure component to the peripheral member 22, wherein the first andsecond force are tangential to the radial direction of eachcorresponding flexure component.

It should be noted one aspect of the invention is use of the flexureassemblies being configured such that on each side of the flexurecomponent they are connected to provide compliance in a direction of thelongitudinal length of the flexure component from the hub to the outerperimeter. The flexible elements of the flexure assemblies are definedby aligned corresponding planes, the planes of which are orthogonal tothe direction of compliance and coincide at least approximately with amidpoint along the length of the corresponding flexure component.Although various embodiments of flexure components such as components31-34 have and will be described, these specific structures should notbe considered the only components that can be used, but rather otherflexure components can be used.

In one embodiment each of the flexure components 31-34 includes sensorelements to measure shear deflection or strain therein. The sensingelements can take any number of forms known to those skilled in the art,including electrically and optically based sensor elements to name justa few. In the embodiment illustrated, strain gauges are connected in aWheatstone bridge with strain gauge elements placed on both sides of theflexure component on the principle stress axis. Referring to theenlarged view of FIG. 5 and the circuit diagram of FIG. 7, theWheatstone bridge 70 includes sensor elements 71 and 72, on one side ofthe flexure component, while on a side opposite of the flexure componentthat is shown in FIG. 5, sensor elements and 73 and 74 (shown withdashed lines) are affixed to the flexure component.

It should be noted in the embodiment illustrated, each of the flexurecomponents 31-34 are relatively thin in a direction parallel to centralaxis 35. However, it should be noted, that the component is not thin inthis direction in order to necessarily provide compliance but rather,the thickness of the flexure components are minimized in order to obtaina high output signal (maximize deflection) and a higher signal to noiseratio. In yet an alternative embodiment illustrated in FIG. 8, theflexure component 31 includes a sensing portion 80 upon where the sensorelements 71 and 72 are disposed (sensor elements 73 and 74 being on theopposite side of sensing portion 80) and portions 82A and 82B that areon opposite sides of sensor portion 80 and are of greater thickness inorder to provide greater stiffness in the direction parallel to thecentral axis 35, while still maintaining required sensitivity in theaxis of measurement.

Another sensor body is indicated at 102 at FIGS. 9-13, which can be usedin place of the sensor body 12, described above, in one exemplaryembodiment. The sensor body 102 has elements similar in function to thatdescribed above with respect to sensor body 12 and has such similarcomponents are identified with the same reference numbers. Asillustrated, the sensor body 102 includes flexure components 31 and 33,intermediate members 41, connecting members 53 and connecting webs55-57. The flexure components 31 and 33 measure forces between thecentral body 20 and the perimeter body 22 for forces in a directionparallel to axis 61. Sensor body 102 however includes flexure structures102 and 104 to transfer forces between the central body 20 and theperimeter body 22 along axis 63. The flexure structures 103 and 104 aredesigned to be substantially stiffer then the flexure components 31 and33 so as to transfer substantially larger forces between the centralbody 20 and the perimeter body 22.

Referring to flexure structure 103 by way of example, each of theflexure structures 103 and 104 include two flexure components 112A and112B extending from the central body 20 to an intermediate member 111.As illustrated, the flexure components 112A, 112B each have alongitudinal axis indicated at 113A and 113B wherein an acute angle 116is formed between the axes 113A, 113B. In the embodiment illustrated,the flexure components 112A, 112B are oriented so as to converge in adirection toward the intermediate member 111; however, in an alternativeembodiment, if desired, an acute angle can be formed between the flexurecomponents with convergence toward the central body 20 rather than theintermediate member 111.

The intermediate member 111 is connected to the perimeter body 22 withflexure assemblies 115A and 115B (herein by example each comprising aconnecting web 117) on opposite sides of the intermediate member 111.The flexure assemblies 115A and 115B are substantially stiff for forcesalong axis 63, but significantly more compliant for forces along axis 61such that these forces are transferred between the central body 20 andthe perimeter body 22 through the flexure components 31 and 33.

In one embodiment each of the pairs of the flexure components 112A, 112Bfor flexure structures 103 and 104 includes sensor elements to measurecomponent deflection or strain therein. The sensor elements can take anynumber of forms known to those skilled in the art, includingelectrically and optically based sensor elements to name just a few. Inthe embodiment illustrated, strain gauges are connected in a Wheatstonebridge with strain gauge elements placed on opposite sides of eachflexure components 112A, 112B. Referring to FIG. 9 and the circuitdiagram of FIG. 13, a Wheatstone bridge 130 includes sensor elements 131and 132 on opposite sides of flexure component 112A, while sensorelements 133 and 134 are on opposite sides of flexure component 112B.FIG. 12 illustrates location of the sensor elements 131 and 133 on thesides of each of the flexure components 112A and 112B (i.e. parallel tothe sides of the sensor body 102, rather than between the sides of thesensor body 102).

Another sensor body is indicated at 202 at FIGS. 14-15, which can beused in place of the sensor body 12, described above, in one exemplaryembodiment. The sensor body 202 has elements similar in function to thatdescribed above with respect to sensor body 12 and sensor body 102 andas such similar elements are identified with the same reference numbers.As illustrated, the sensor body 202 includes flexure components 31 and33, intermediate members 41, connecting members 53 and connecting webs55-57. The flexure components 31 and 33 measure forces between thecentral body 20 and the perimeter body 22 for forces in a directionparallel to axis 61. Sensor body 202 however includes flexure structures203 and 204 to transfer forces between the central body 20 and theperimeter body 22 along axis 63. The flexure structures 203 and 204 aredesigned to be substantially stiffer then the flexure components 31 and33 so as to transfer substantially larger forces between the centralbody 20 and the perimeter body 22.

Each of the flexure structures 203 and 204 include a flexure component212 that is rectangular (preferably square) in cross-section along thelength thereof, but at least two sides, preferably opposite to eachother, are tapered along the length of the flexure component 212 suchthat one end portion of the flexure component 212 is smaller incross-section than the other end portion, herein end portion 212Aconnected to intermediate member 111 is smaller in cross-section (beforeconnection to intermediate member 111). In the illustrated embodimentall sides are tapered along the length of the flexure component 212,i.e. being frusto-pyramidal in a center section. This constructionallows the strain field in the center of the flexure component 212 to beapproximately 80% (although this value is adjustable based on the shapeof the flexure component 212) of the strain in the connecting fillets atthe ends of the flexure component 212. Each of the sides of the flexurecomponent 212 can include a sensor element such as those described aboveconnected in a conventional Wheatstone bridge (not shown). Strain gauges231 and 232 are illustrated by way of example.

Yet another sensor body is indicated at 242 at FIGS. 16-21, which can beused in place of the sensor body 12, described above, in one exemplaryembodiment. The sensor body 242 has elements similar in broad functionto that described above with respect to sensor body 12 and as suchsimilar elements are identified with the same reference numbers. Asillustrated, the sensor body 242 includes flexure components 251 and253, intermediate members 41, connecting members 53 and connecting webs55-57. The flexure components 251 and 253 measure forces between thecentral body 20 and the perimeter body 22 for forces in a directionparallel to axis 61. In this embodiment, flexure components 252 and 254,intermediate members 41, connecting members 53 and connecting webs 55-57measure forces between the central body 20 and the perimeter body 22 forforces in a direction parallel to axis 63 and are also substantially thesame as the flexure structures for measuring forces in a directionparallel to axis 61. However, this is not a requirement as demonstratedby the previous embodiments. Hence, any of the other flexure structurescan be used, typically in pairs, but otherwise without limitation, ofany of the previous embodiments for either measuring forces in adirection parallel to axis 61 or to axis 63.

In the embodiment of FIGS. 16-21, the flexure components 251-254 arevery similar to flexure components 31-34; however, flexure components251-254 include corresponding apertures 251A, 252A, 253A and 254A. Thestrain gauges on the flexure components 251-254 are configured tomeasure strain in bending (as parallel double cantilever bending beams255A and 255B illustrated in FIG. 20) rather than to measure strain inshear as flexure components 31-34 operate. Each of the flexurecomponents 251-254 includes sensor elements to measure bendingdeflection or strain therein. The sensing elements can take any numberof forms known to those skilled in the art, including electrically andoptically based sensor elements to name just a few. For instance,resistive strain gauges connected in a suitable Wheatstone bridge can besecured to each of the beams 255A and 255B of each flexure component251-254. In one embodiment, the strain gauges are secured to theinwardly facing surface 254B of each beam 255A, 255B formed by eachaperture 251A-254A, although the strain gauges could also be secured tothe outwardly facing surfaces 254C, which face in opposite directions.Like the flexure components 31-34, the sensing gauges for sensingdeflection of each of the beams 255A and 255B are located approximatelyat the midpoint of each beam 255A, 255B of each flexure component251-254 and where the flexible elements (connecting members 53 andconnecting webs 55-57) of the flexure assemblies are defined by alignedcorresponding planes, the planes of which are orthogonal to thedirection of compliance and coincide at least approximately with amidpoint along the length of each beam 255A, 255B of the correspondingflexure component 251-254, or stated another way bisect each of theapertures 251A-254A. The structure of the flexure components 251-254provides high stiffness with very good resolution and low cross-talk.Although apertures 251-254 are illustrated as round holes, it should beunderstood that the apertures could be of any suitable shape, such asbut not limited to square apertures with rounded corners, or the like,without departing from the scope of the disclosure.

An exemplary embodiment of any of the foregoing transducer bodies withsuitable sensing elements to form a transducer assembly can beincorporated in a platform balance 300 an example of which isillustrated in FIGS. 22-23. In the embodiment illustrated, the platformbalance 300 can include a first frame support 302 and a second framesupport 304. A plurality of transducer assemblies 340A-D, herein fouralthough any number three or more can be used, couple the first framesupport 302 to the second frame support 304. The platform balance 300can be used to measure forces and moments applied to a test specimen ofnominally large weight or mass such as a vehicle, plane, etc. or modelsthereof. The frame supports 302 and 304 are nominally unstressedreaction frames, wherein each of the transducers comprises a two-axisforce transducer as described above. Various levels of flexure isolationcan be provided in the platform balance 300 to provide increasedsensitivity, while nominally supporting large masses.

The platform balance 300 is particularly well suited for measuring forceand/or moments upon a large specimen such as a vehicle in an environmentsuch as a wind tunnel. In this or similar applications, the platformbalance 300 can include flexures 315 isolating the frame support 302 and304 from the test specimen and a ground support mechanism. In theembodiment illustrated, four flexures 315 are provided between each ofthe transducer assemblies, being coupled to the plates 320. Similarly,four flexures 324 are coupled to the mounting plates 322. The flexures315, 324 thereby isolate the frame supports 302 and 304. The flexures315, 324 are generally aligned with the sensor bodies of eachcorresponding transducer assembly.

The platform balance 300 is particularly well suited for use inmeasuring forces upon a vehicle or other large test specimen in a windtunnel. In such an application, rolling roadway belts 332 are supportedby an intermediate frame 334 coupled to the flexure members 315. Therolling roadway belts 332 support the vehicle tires. In someembodiments, a single roadway belt is used for all tires of the vehicle.The platform balance 300 and rolling roadway belt assemblies 332 arepositioned in a pit and mounted to a turntable mechanism 336 so as toallow the test specimen, for example a vehicle, to be selectively turnedwith respect to the wind of the wind tunnel.

Each of the frame supports 302 and 304 comprise continuous hollow boxcomponents formed in a perimeter so as to provide corresponding stiffassemblies. The frame support 302 holds the sensor bodies in positionwith respect to each other, while the frame support 304 holds the clevisassemblies in position with respect to each other. Stiffening box framemembers 333 can also be provided in the support frame as illustrated.

As appreciated by those skilled in the art, outputs from each of thetwo-axis sensing circuits from each of the transducer assemblies can becombined so as to sense or provide outputs indicative of forces andmoments upon the platform balance in six degrees of freedom. Acoordinate system for platform 300 is illustrated at 331. Output signalsfrom transducer assemblies 340A and 340C are used to measure forcesalong the X-axis, because transducer assemblies 340B and 340D arecompliant in this direction. Likewise, output signals from transducerassemblies 340B and 340D are used to measure forces along the Y-axis,because transducer assemblies 340A and 340C are compliant in thisdirection. Outputs from all of the transducers 340A-340D are used tomeasure forces along the Z-axis. The flexure components 251-254 arerelatively stiff or rigid for lateral loads, that being in a directionparallel to axis 62. Overturning moments about the X-axis are measuredfrom the output signals from transducers 340A and 340C; whileoverturning moments about the Y-axis are measured from the outputsignals from transducers 340B and 340D; and while overturning momentsabout the Z-axis are measured from the output signals from transducers340A-340D. Processor 380 receives the output signals from the sensingcircuits of the transducers to calculate forces and/or moments asdesired, typically with respect to the orthogonal coordinate system 331.

If desired a counter balance system or assembly can be provided tosupport the nominal static mass of the test specimen, other componentsof the operating environment such as roadways, simulators and componentsof the platform balance itself. The counter balance system can take anyone of numerous forms such as airbags, hydraulic or pneumatic devices,or cables with pulleys and counter weights. An important characteristicof the counter balance system is that it is very compliant so as not tointerfere with the sensitivity or measurement of the forces by thetransducer assemblies in order to measure all of the forces and momentsupon the test specimen. In the embodiment illustrated, the counterbalance system is schematically illustrated by actuators 330.

However, in a further aspect of the present invention, the counterbalance system can be removed as explained below, which can be a verylarge cost savings. Referring back to FIGS. 16 and 18, the sensor body242 includes a biasing structure 402 disposed on the sensor body 242 soas to develop a biasing offset force in a selected direction, herein byway of example along the axis 63 in the Z-direction. The biasingstructure 402 comprises cantilevered beams 404A and 404B. In theembodiment illustrated, remote ends 406A and 406B extend in oppositedirections where each of the beams 404A and 404B are mounted to thesensor body 242 by a base support 408. It should be noted that use of asingle base support 408 is not necessary in that the cantilevered beams404A and 404B can each have a separate base support secured to sensorbody 242; however use of a single base support 408 is of a simplerconstruction. Likewise, although illustrated with the beams 404A and404B extending in opposite directions alternative embodiments may havethe beams extend toward each other. Finally, the biasing structure 402need not be a cantilevered beam, but can be any structure that isconfigured to provide a biasing force for the purpose described below.

In the embodiment illustrated the biasing structure 402 can be formedintegral with the sensor body 242 from a single unitary body; however,this should not be considered limiting in that individual components canbe joined together and/or joined to the sensor body 242 to realize thesame structure.

Referring also to FIGS. 24 and 25, biasing retaining elements 418connect the biasing structure 402 (located between the clevis halves 16and 18) to the clevis halves 16 and 18. In the embodiment illustrated,the biasing retaining elements 418 operate in tension and hereincomprise elongated connectors 420 each joined at a first end 420A to oneof the remote ends 406A or 406B with a suitable fastener herein bolts422. A second end 420B of the elongated connectors 420 is joined to bothof the clevis halves 16 and 18, herein by a bridging block 424separately connected to each of the clevis halves 16 and 18 with asuitable fastener herein bolts 426.

Biasing retaining elements 418 in one embodiment comprise straps orflexible members. As shown, straps 418, under tension, are coupled atone end 420A to a cantilevered beam at its remote end, and are coupledat the other end 420B to bridging block 424 coupled to clevis halves 16and 18. Together, the biasing elements 418, bridging block 424, andfasteners such as 422 and 426 comprise a biasing assembly connectedbetween the support (clevis halves 16 and 18) and the sensor body 12 toprovide a bias force between the sensor body 12 and the clevis halves.As shown, a width 423 of the straps 418 is greater than a thickness 425of the straps 418. A biasing assembly in one embodiment comprises a pairof straps provided on opposite portions of the transducer body that aresymmetric in configuration, to allow for compliance in a directionorthogonal to the offset. For example only and not by way of limitation,the straps 418 may have a square cross-section, that is, an equal width423 and thickness 425, or cylindrical, with a constant diameter in everycross-section direction, or other symmetric configurations such as willbe evident to those of skill in the art.

A biasing actuator 432 (illustrated schematically with dashed lines)preloads the biasing structure 402 and in particular bends thecantilevered beams 404A and 404B by pulling on the bridging block 424upwardly with the biasing actuator 432 operably connected to standoffs434. Any form of actuator can be used such as but not limited to ahydraulic, electric, etc. In one embodiment the actuator 432 comprises ascrew or bolt mechanically connecting the standoffs 434 with thebridging block 424.

A biasing force can be provided as follows. With a loose connection ofthe bridging block 424 to the clevis halves 16 and 18, each biasingactuator 432 on each side of the sensor body 242 is operated to obtainthe desired preloading on the biasing structure 402 as a whole at whichpoint the bridging blocks 424 are then securely fixed to the clevishalves 16 and 18 to retain the desired bias force. In one embodiment,the bias force from each cantilever 404A and 404B is iterativelyincreased until the desired bias force is obtained. The contribution ofthe bias force from each cantilever 404A and 404B should be the same soas to not induce a moment in the sensor body 242, but rather provide apurely linear bias force in a direction parallel to axis 63 in theillustrated embodiment.

It should be noted that the biasing structure need not be provided onthe sensor body 242, or only on the sensor body 242. FIGS. 26-28illustrate a transducer assembly 500 having many of the same componentsof the previous transducer assembly, which have been identified with thesame reference numbers. In this embodiment though, additional biasingstructures 502 have been formed on each of the clevis halves 16 and 18.The biasing structure 502 is similar to biasing structure 402 discussedabove; and thus, much if not all the discussion applicable to biasingstructures 402 is applicable to biasing structures 502. For example, inone embodiment, cantilevered beams 504A and 504B and a single basesupport 508 are integrally formed from a single unitary body; however,this is but one embodiment, where other structures as described abovewith respect to biasing structure 402 can also be used.

Referring to FIG. 28, biasing retaining elements 518 connect the biasingstructures 502 to the to the sensor body 242. In the embodimentillustrated, each of the biasing retaining elements 518 operate intension and herein comprise elongated connectors 520 with a first endhaving a bridging block 524 at a first end 520A connecting the remoteends 506A or 506B together with a suitable fastener herein bolts 522. Asecond end 520B of each of the elongated connectors 520 is joined to thesensor body 242, with a suitable fastener herein bolts 526. Biasingretaining elements 518 in one embodiment have the properties andcharacteristics described above with respect to biasing elements 418.

In this embodiment, sensor body 242 also includes biasing structure 402having similar components identified with the same reference numbers. Abiasing actuator not shown but connectable in a manner similar to thatdescribed above and is in effect removably connected to each of thebeams 404A, 404B so as to pull the beams 404A, 404B upwardly in FIG. 28at which point the retainer 418 is securely fixed to retain the biasforce such as by securely fixing the bridging block 424 to the sensorbody 242. In a similar manner, a biasing actuator not shown butconnectable in a manner similar to that described above and is in effectremovably connected to each of the beams 504A of each clevis 16, 18 soas to pull the beams 504A or 504B in pairs on each side of thetransducer 500 using corresponding bridging blocks 524 and suitablestandoffs as needed. When the desired bias force is obtained in eachpair of beams 504A and 504B, the associated end 520B of the biasretainer 518 can be securely fixed to the sensor body 242. As in theprevious discussion of bias structure 402, any form of actuator can beused such as but not limited to screws or bolts, hydraulic, electric,etc.

An overtravel stop can be provided to limit the bias force created bythe pairs of beams 504A and 504B on the clevis halves 16 and 18.Referring to FIGS. 29 and 30, a bolt 550 is secured to support 408 andextends through an aperture 552 provided in element 17 connecting theclevis halves 16, 18 together. The head of the bolt 550 is of size to belarger than the aperture 552. The bolt 552 is secured to the support 408with the head of the bolt spaced apart from a surface of the connectingelement a selected distance corresponding to a limit of bias force to begenerated by beams 504A and 504B. Since loading of beams 504A and 504Bcauses the sensor body 242 to move upwardly in FIG. 29, contact of thehead of the bolt 552 limits the bias force that can be generated.

Another aspect of the present invention is a lock up assembly 600 thatselectively secures the position of the sensor body 12 relative to theclevis halves 16 and 18. Referring to FIGS. 31 and 32, the lock upassembly 600 includes friction plates 602 attached to each of the clevishalves. Each friction plate 602 is attached to its corresponding clevishalf with a fastener 604 such as a plurality of fasteners in the centerof the plate. However, it should be noted that only the center of theplate is in permanent contact with the corresponding clevis halves inthat the extending ends 606 of the friction plates 602 are spaced apartfrom the outer surface of the corresponding clevis half. A spacer 608 issecurely fixed to the sensor body and is disposed between ends 606 ofthe friction plates 602 on each side of the transducer. The length ofthe spacer 608 is slightly shorter than the distance between the innersurfaces of the friction plates such that a gap 610 is present betweenone or both of the end surfaces of the spacer 608 and correspondinginwardly facing surfaces 612 of the friction plates 602. An actuator 614is operably coupled to the friction plates 602. The actuator 614includes a pull rod 616 that extends through a bore 618 in the spacer.The bore 618 is of size to maintain a gap between the pull rod 616 andthe spacer 618 for movements of the sensor body 12 or the clevis halves16 and 18 relative to the sensor body 12. When it is desired to inhibitmovement of the sensor body 12 relative to the clevis halves 16 and 18,the actuator 614 is operated so as to retract the pull rod 616 whichpulls the ends 606 of the friction plates 602 together therebyeliminating the gap(s) 610 between the end surface(s) of the spacer 608and the inwardly facing surface(s) 612 of the friction plates 602 aswell as eliminating the gap(s) 620 between the inwardly facingsurface(s) 612 of the friction plates 602 and the outwardly facingsurface 622 of each corresponding clevis half. As such, when theactuator 614 is operated, a solid connection is formed between thespacer 608 and the friction plates 602 wherein the friction plates 602frictionally engage the outer surfaces 622 of each corresponding clevishalf.

The actuator 614 can be of any suitable form such as but not limited toan electric, hydraulic, or pneumatic actuator.

In the embodiment illustrated, each of the friction plates 602 includesareas of reduced thickness that form flexible hinges 624. The flexiblehinges 624 ensure that the ends 606 of the friction plates 602 willmaximize contact of the end surfaces of the friction plates 602 with theclevis halves 16 and 18 rather than being slightly at an angle if theflexible hinges 624 were not present. In other words, the portion of thefriction plates 602 that secure the friction plates 602 to the clevishalves by the fasteners indicated at 604 is maintained in a planarfashion to the corresponding clevis halves. Likewise, when the actuator614 is operated, each of the end portions 606 of the friction plates 602will contact the corresponding clevis half in a planar fashion. Anyslight difference in width between the center sections of the frictionplates 602 and the end portions of the friction plates 602 isaccommodated by the middle sections between each of the flexible hinges624.

The embodiments pre-loading the transducer body with respect to theclevis plates, as shown and described above, allow for accurate fullscale measurement even if the tare weight placed on the platform 300 ismany times a full scale measure load weight. For example, a 20,000 poundupper frame is supportable with four transducer bodies while stillallowing accurate measurement of loads in a full scale measure load of+/−2,000 pounds vertical, without frequency degradation of a dead-weighttype tare system. Such embodiments are amenable to use with other loadcells where tare mitigation is employed, without departing from thescope of the disclosure.

In such a pre-loading, thermal expansion differences can lead to thermalstructural temperature equilibration between components of thetransducer body and any sensing elements therein. Thermal expansiondifferences between, for example, parallel springs (e.g., thecantilevered beams) in series with straps and those in parallel withgauged beam assemblies, and the resulting disparate temperatures betweenelements, may result in thermal drift for a duration of a test.

FIG. 33 shows a fluid enclosure 700 for a transducer assembly such asthe various transducer assembly embodiments described herein. In oneembodiment, fluid enclosure 700 is an oil enclosure or oil bath, such asa fluid recirculating bath assembly. Elements of the transducer,especially straps, cantilevered beams, gauged elements, sensor body,clevis plates, and bottom plates, are immersed in the fluid of the fluidenclosure 700, and are held in one embodiment to a same temperature witha tolerance of about 0.1° F. for a testing cycle. In one embodiment,fluid enclosure 700 contains an oil 702 heated to a desired temperatureat which the elements of the transducer are to be held. Oil 702 has highthermal mass and very good heat conduction and convection to and withthe elements of the transducer assembly. This allows maintenance ofthermal uniformity within a desired tolerance even when the transducerassembly is in an operating wind tunnel.

Oil enclosure 700 further comprises cross flow inlets 704 and outlets706, and a fluid circulating bath tank 708 mounted to a plate 710. Agasket 712 seals tank 708 to plate 710 in one embodiment. Furthergaskets 714 may be used to seal plate 710 to a bottom plate such asconnecting member 17 of a transducer body (FIG. 1), for example bysealing each bolt between bottom flexures 716 and connecting member 17,or by sealing with a larger gasket around a circumference of the bottomflexures 716. Top flexures 718 may be coupled, for example with bolts,to the sensor body of the transducer assembly. Associated plumbing (notshown) provides oil 702 at the desired temperature for the components tothe enclosure 700 via inlets 704, recirculated to the plumbing andheater (not shown) via outlets 706. A top cover 720, shown in FIG. 34,may be used to provide protection against contaminants such as dirt ordust into the tank 708. In one embodiment, oil is provided to fill tank708 to fill line 722, so that sensing elements that may be in thetransducer body are completely submerged in the oil.

Although the subject matter has been described in language specific tostructural features and/or methodological acts, it is to be understoodthat the subject matter defined in the appended claims is notnecessarily limited to the specific features or acts described above ashas been held by the courts. Rather, the specific features and actsdescribed above are disclosed as example forms of implementing theclaims.

What is claimed is:
 1. A platform balance suitable for transmittingforces and moments in a plurality of directions, the platform balancecomprising: a frame support; and at least three spaced-apart transducerbodies coupled to the frame support, each transducer body comprising: asupport comprising a pair of clevis halves; and a sensor body coupled toeach of the clevis halves, wherein the sensor body is disposed betweenthe clevis halves and configured to deflect with forces along twoorthogonal axes, wherein the sensor body includes a generally rigidperipheral member disposed about a spaced-apart central hub, the centralhub being joined to each of the clevis halves with the peripheral memberspaced apart from each clevis half, wherein at least three flexurecomponents couple the peripheral member to the central hub, and whereinthe flexure components are spaced-apart from each other at generallyequal angle intervals about the central hub; the sensor body furtherincluding a flexure assembly for each of said at least some flexurecomponents joining the flexure component to at least one of the centralhub and the peripheral member, the flexure assembly being compliant forforces in a radial direction from the central hub through the flexurecomponent and to the peripheral member, wherein each flexure assembly isconfigured such that forces transferred between central hub and theperipheral member concentrate strain at a midpoint along the length ofeach corresponding flexure component.
 2. The platform balance of claim 1wherein each flexure assembly is configured such that forces transferredbetween central hub and the peripheral member cause a first force at theconnection of the flexure component to the central hub to be equal andopposite to a second force at the connection of the flexure component tothe peripheral member, wherein the first and second force are tangentialto the radial direction of each corresponding flexure component.
 3. Theplatform balance of claim 1 wherein said at least some of the flexurecomponents are configured to concentrate strain in shear.
 4. Theplatform balance of claim 1 wherein said at least some of the flexurecomponents are configured to concentrate strain in bending.
 5. Theplatform balance of claim 1 wherein said at least some of the flexurecomponents are configured with a pair of beams.
 6. The platform balanceof claim 5 wherein the pair of beams of each flexure component of atleast some of the flexure components is formed by an aperture.
 7. Theplatform balance of claim 1, and further comprising: a biasing assemblyconnected between the support and the sensor body and configured toprovide a bias force between the sensor body and the support.
 8. Theplatform balance of claim 7 wherein the biasing assembly comprises abias connector configured to operate in tension to provide the biasforce.
 9. The platform balance of claim 8 wherein the bias connectercomprises an elongated strap having a width of the strap greater than athickness of the strap.
 10. The platform balance of claim 9 wherein thebiasing assembly comprises a pair of straps provided on oppositeportions of the transducer body that are symmetrical.
 11. The platformbalance of claim 10 wherein the biasing connector comprises a flexiblemember fixedly connected to one of the sensor body or the support. 12.The platform balance of claim 11 wherein the flexible member isintegrally formed from a single unitary body of one of the sensor bodyor the support.
 13. The platform balance of claim 9 wherein the biasingassembly comprises a pair of biasing connectors wherein a biasingconnector is provided each of opposite portions of the transducer bodythat are symmetrical.
 14. The platform balance of claim 13 wherein thebiasing structure comprises flexible members, a flexible member beingfixedly connected to one of the sensor body or the support.
 15. Theplatform balance of claim 14 wherein the flexible members are integrallyformed from a single unitary body of one of the sensor body or thesupport.
 16. The platform balance of claim 11 wherein each flexiblemember comprises a cantilevered beam with one of the biasing connectorsconnected to one of the flexible members.
 17. The platform balance ofclaim 12 wherein the flexible member is provided on the support.
 18. Theplatform balance of claim 13 wherein a flexible member is provided oneach clevis half and a bridging block connects the flexible portionstogether, the bridging block being spaced apart from the sensor body.19. The platform balance of claim 12 wherein the flexible portion isprovided on the sensor body.
 20. The platform balance of claim 8 whereinthe biasing assembly comprises a removable biasing actuator configuredto be connected between the sensor body and the support.
 21. Theplatform balance of claim 1, and further comprising: a lockup assemblyconfigured to selectively inhibit movement of the sensor body relativeto the clevis halves.
 22. The platform balance of claim 21 wherein thelockup assembly is configured to inhibit movement of the peripheralmember relative to the clevis halves.
 23. The platform balance of claim22 wherein the lockup assembly inhibits movement of the peripheralmember by frictional contact.
 24. The platform balance of claim 23wherein the lockup assembly is configured to selectively move portionshaving engaging surfaces for frictional contact to contact opposedsurfaces of the peripheral member, the engaging surfaces and the opposedsurfaces being spaced apart from each other to allow forces to betransferred by the flexure components when the lockup assembly is notengaged.
 25. The platform balance of claim 24 wherein the lockupassembly comprises a first plate member jointed to a first clevis halfand a second plate member joined to the second clevis halve, wherein theengaging surfaces are disposed on the plate members.
 26. The platformbalance of claim 25 wherein a portion of each plate member is spaceapart from the associated clevis half.
 27. The platform balance of claim26 wherein when the engaging surface engage the opposed surfaces, theportion of each plate member frictionally engages the associated clevishalf.
 28. The platform balance of claim 27 and further comprising anactuator configured to selectively bring the engaging surfaces incontact with the opposed surfaces and also bring the portions of eachplate member into contact with each associated clevis half.
 29. Theplatform balance of claim 28 wherein major surfaces of the portions ofthe plate members engage major surfaces of the associated clevis halves.30. The platform balance of claim 29 wherein the engaging surfaces areon the plate members, and wherein each plate member comprises a hingesand a link portion between the hinges, the link portion connectingportions of the plate members having the engaging surfaces with portionsof the plate members having the major surfaces.
 31. The platform balanceof claim 30 wherein the actuator is operably mounted to the portions ofthe plate members having the engaging surfaces, and wherein the actuatorincludes a pull rod to selectively pull the pull rod so as to bring theengaging surfaces in contact with the opposed surfaces.
 32. The platformbalance of claim 31 wherein the pull rod extends through a bore openingto one of the opposed surfaces, the pull rod being spaced apart frominner surfaces of the bore at least when the actuator is not pulling onthe pull rod to bring the engaging surfaces in contact with the opposedsurfaces.
 33. A platform balance suitable for transmitting forces andmoments in a plurality of directions, the platform balance comprising: aframe support; and at least three spaced-apart transducer bodies coupledto the frame support, each transducer body comprising: a supportcomprising a pair of clevis halves; and a sensor body coupled to each ofthe clevis halves, wherein the sensor body is disposed between theclevis halves and includes a generally rigid peripheral member disposedabout a spaced-apart central hub, the central hub being joined to eachof the clevis halves with the peripheral member spaced apart from eachclevis halve, wherein at least three flexure components couple theperipheral member to the central hub, and wherein the flexure componentsare spaced-apart from each other at generally equal angle intervalsabout the central hub; and a biasing assembly connected between thesupport and the sensor body and configured to provide a bias forcebetween the sensor body and the support.
 34. A platform balance suitablefor transmitting forces and moments in a plurality of directions, theplatform balance comprising: a frame support; and at least threespaced-apart transducer bodies coupled to the frame support, eachtransducer body comprising: a support comprising a pair of clevishalves; and a sensor body coupled to each of the clevis halves, whereinthe sensor body is disposed between the clevis halves and includes agenerally rigid peripheral member disposed about a spaced-apart centralhub, the central hub being joined to each of the clevis halves with theperipheral member spaced apart from each clevis halve, wherein at leastthree flexure components couple the peripheral member to the centralhub, and wherein the flexure components are spaced-apart from each otherat generally equal angle intervals about the central hub; and a lockupassembly configured to selectively inhibit movement of the sensor bodyrelative to the clevis halves.